Title (fr)

Publication

Application

Priority

US 9606426 W 19960508

US 44053695 A 19950512

Abstract (en)

[origin: WO9635957A1] A gimballed vibrating wheel gyroscope (10) for detecting rotational rates in inertial space. The gyroscope (10) includes a support (20) oriented in a first plane and a wheel assembly (12) disposed over the support (20) parallel to the first plane. The wheel assembly (12) is adapted for vibrating rotationally at a predetermined frequency in the first plane and is responsive to rotational rates about a coplanar input axis (32) for providing an output torque about a coplanar output axis (34). The gyroscope (10) also includes a post assembly (18a, 18b) extending between the support (20) and the wheel assembly (12) for supporting the wheel assembly (12). The wheel assembly (12) has an inner hub (24), an outer wheel (26), and spoke flexures (28a-28d) extending between the inner hub (24) and the outer wheel (26) and being stiff along both the input and output axes (32, 34). A flexure (22a, 22b) is incorporated in the post assembly (18a, 18b) between the support (20) and the wheel assembly inner hub (24) and is relatively flexible along the output axis (34) and relatively stiff along the input axis (32).